View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 20852U 90081Q 24277.67473145 .00010564 00000-0 45835-2 0 9997
2 20852 98.6465 262.1919 0015333 233.3798 126.5972 14.24281622757134
| Epoch (UTC): | 03 October 2024 16:11:36 |
| Eccentricity: | 0.0015333 |
| inclination: | 98.6465° |
| perigee height: | 800 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 262.1919° |
| argument of perigee: | 233.3798° |
| revolutions per day: | 14.24281622 |
| mean anomaly at epoch: | 126.5972° |
| orbit number at epoch: | 75713 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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